F-1
Multipurpose fighter

	Specification:
	Year deployed Wing span, m Lenght, m Height, m Wings area, m2 Weight, kg - maximum take-off - empty operating  fuel, l - Internal - AFT Engines Thrust, kN (kgs) - dry - afterburner Maximum speed, km/h - in altitude - on sea level Rate of climb, m/min Range, km Combat radius, km Service ceiling, m Armament:	- 1977 - 7.88 - 17.86 - 4.39 - 21.18 - 13675 - 6360 - 3823 - 3 У 821 - 2 TSEA Ishikawajima-Harima TF40-IHI-801A (Rolls-Royce Adour Mk.801A) - 2 У 22.75 (2320) - 2 У 32.49 (3315) - 1700 (M=1.6) - - 10670 - 2600 - 555 -15240 20 -mm six-barrel cannon JM61 (M61 Vulcan) with 750 rounds . Warload - 2780 kg in 7 hardpoints 4 AAM AIM-9 Sidewinder or AюM-1 or 2 anti-ship missile ASM-1 (Type 80) or 9 340 kg bombs or 12 227(113) kg bombs or  4 ML 7У70-mm(RL-7) 19У70-mm(LAU-3/A)  or 4 4У127-mm(RL-4) UR